Analysis of Flow Evolution and Thermal Instabilities in the Near-Nozzle Region of a Free Plane Laminar Jet

Table 1

Algorithm steps.

Step	Computed or updated variable	By applying
1	, , and	, , and
2	Temperature	Equation (3)
3	Intermediate density	Equation (6)
4	Intermediate velocity	Equation (2)
5	Pressure correction	Equation (8)
6	Pressure
7	Corrected density	Equation (6)
8	Corrected velocity

The convergence is verified by the averaged L2 norm as follows: if is false, then and return to Step 2; else, and proceed to next time step (Step 1). Here and .